Computational study of high-angle-of-attack missile flows using two-equation turbulence models
36th AIAA Aerospace Sciences Meeting and Exhibit ; 1998 ; Reno , NV , U.S.A.
1998-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Computational Investigations of Subsonic High Angle of Attack Missile Flows
British Library Conference Proceedings | 1998
|Application of Turbulence Models to Separated High-Angle-of-Attack Flows
British Library Conference Proceedings | 1998
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